Process Characterization of Low Speed, Fiber Laser Welding of AA 7075-T6 - Application to Fatigue Crack Repair.

Show simple item record

dc.contributor.advisor Dr. Pierre A. Gremaud, Committee Member en_US
dc.contributor.advisor Dr. Kara J. Peters, Committee Member en_US
dc.contributor.advisor Dr. Clement Kleinstreuer, Committee Member en_US
dc.contributor.advisor Dr. Juei-Feng Tu, Committee Chair en_US
dc.contributor.author Paleocrassas, Alexander Grant en_US
dc.date.accessioned 2010-04-02T19:01:13Z
dc.date.available 2010-04-02T19:01:13Z
dc.date.issued 2009-04-21 en_US
dc.identifier.other etd-03262009-102830 en_US
dc.identifier.uri http://www.lib.ncsu.edu/resolver/1840.16/4796
dc.description.abstract Aluminum alloys are widely used in the aerospace industry as structural materials, mainly due to their high strength to weight ratio. However, fatigue-induced cracks start to appear on aircraft components and, unless replaced or repaired, propagate to critical lengths which may result in catastrophic failure. A method that is being considered for crack repair is fusion (welding). However, aluminum alloys are some of the most challenging metals to weld successfully. Since cracks do not propagate in straight lines low speed welding is required to avoid high acceleration and deceleration effects. A process characterization was performed investigating low speed welding from 10 mm/s down to 1 mm/s. Results showed that the welding followed the expected trend until the speed dropped below a threshold (~ 1 mm/s) at which there was a significant change in the process, causing shallow, inefficient welds with many defects. Experimental evidence suggested that a large molten pool is created at low speeds. As a result, the CW laser beam mainly irradiates at the molten pool, which absorbs a large portion of the beam energy near the surface, and subsequently transfers the energy into the bulk material via more effective convection and conduction. Consequently, the welding process becomes inefficient and the welds become shallow and wide. Pulsed welding was tested as part of a hypothesis to improve the Fresnel absorption (multiple reflections) and therefore achieve deeper weld penetration without overheating the molten pool. Results showed that decreasing the average power by pulsing creates a much more efficient process; however, solidification cracking became a problem. Therefore, the best CW welding condition was applied to thinner sheets for full penetration welding and crack repair. Tensile tests showed that the best ultimate strength recovery was about 75% percent of the base material. This result is highly encouraging, considering the alloy is only 50% as strong before heat treatment. In combination with a composite patch this process might prove to be a viable solution for fatigue crack repair. en_US
dc.rights I hereby certify that, if appropriate, I have obtained and attached hereto a written permission statement from the owner(s) of each third party copyrighted matter to be included in my thesis, dis sertation, or project report, allowing distribution as specified below. I certify that the version I submitted is the same as that approved by my advisory committee. I hereby grant to NC State University or its agents the non-exclusive license to archive and make accessible, under the conditions specified below, my thesis, dissertation, or project report in whole or in part in all forms of media, now or hereafter known. I retain all other ownership rights to the copyright of the thesis, dissertation or project report. I also retain the right to use in future works (such as articles or books) all or part of this thesis, dissertation, or project report. en_US
dc.subject fatigue crack repair en_US
dc.subject low speed en_US
dc.subject aluminum en_US
dc.subject laser welding en_US
dc.subject fiber laser en_US
dc.title Process Characterization of Low Speed, Fiber Laser Welding of AA 7075-T6 - Application to Fatigue Crack Repair. en_US
dc.degree.name PhD en_US
dc.degree.level dissertation en_US
dc.degree.discipline Mechanical Engineering en_US


Files in this item

Files Size Format View
etd.pdf 2.467Mb PDF View/Open

This item appears in the following Collection(s)

Show simple item record